The proposed model is performed according to the scheme “duck”. The stabilizer is located in front of the wing, contributes to the sustainability planning mode. A deviation to vertical position after deployment, a simple “timer” (wick device ignites the expelling charge motor) ensures a safe landing apparatus.
The Central beam rocket hewed out of pine and has a cross section of 4X4 mm. In its nasal part of the thread with glue is attached to the spring hinges, bearing side beams of variable cross section. In addition, 80 mm from the front end of the Central beam pivotally mounted node of the beam stabilizer (pine section of 3X4 mm). In the middle of the last bound rubber band to hold the stabilizer at a predetermined angle of attack. She passed through the ring of the spring hinge and ends of cotton thread No. 10 or No. 5 with a length of 100 mm with a knot at the end. When equipped model, the pull to the tail end of the Central beam and grab the wick with a nylon thread No. 50. Hold the stabilizer in a vertical position during the transition from planning to forced descent is provided by knot in the middle of the elastics, the value of which does not allow him to slip through the ring joint. Stitched wing and stabilizer used Mylar film thickness of 3-6 microns. The mass of the rocket is 18.5 g.